TECNAM P2012 TRAVELLER

TECNAM

P2012 TRAVELLER

New

0

0

SNEW

2000

Lycoming TEO-540-C1A: 6-cylinder, horizontally opposed, turbocharged, air-cooled engine. Electronic fuel injection, electronic ignition, down exhaust. The engine has an automotive type starter, one 28V alternator (140A) and a propeller governor pad. EECS (Electronic Engine Control): Continuously monitors and adjusts ignition timing, fuel injection timing, and fuel mixture based on operating conditions eliminating the need for magnetos and manual fuel/air mixture control lever. Fuel: (Min Octane) 100/130, 100LL and UL100 Fuel Scheduling/Mapping: Changeable in Software Time limited takeoff rating: Anticipated in Software 1 x Alternator – 28 Volt, 140 Amp Engine Protection Systems & Diagnostics Knock Control (independent for each cylinder) CHT, TIT over temp protection – Overspeed protection– Overboost protection Notification of Shorted/Open Sensor or Actuators Out-of Range Failures In-Range Errors from sensor (Cross Checks) Pilot Interface All faults are logged in the ECU memory Service Fault History Record since last clearing by an authorized service tool Record of ’’Fault clearing History’’

Garmin G1000 Nxi, composed of two 10 inch PFDs Single central 12 inch MFD. Remote redundant AHRS and ADC (inertial and air data units) provide the main flight and attitude information whilst a backup is provided by a small, vertical layout MD-302 (Mid-Continent). Communications and navigation are based on dual remote units which provide selectable data on the cockpit screens. An optionally provided Flight Management System keyboard allows immediate and comfortable insertion of frequencies and waypoints, while another optionally provided Garmin Flight Stream device allows an immediate and wireless link between flight suite and portable devices such as tablets or smartphones for immediate introduction of flight plans, waypoints, routes, frequencies etc…